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Global fast terminal sliding mode control for automatic carrier landing with environmental disturbances

Zhuoer Yao (School of Aeronautic Science and Engineering, Beihang University, Beijing, China)
Zi Kan (School of Aeronautic Science and Engineering, Beihang University, Beijing, China)
Daochun Li (School of Aeronautic Science and Engineering, Beihang University, Beijing, China and Tianmushan Laboratory, Hangzhou, China)
Haoyuan Shao (School of Aeronautic Science and Engineering, Beihang University, Beijing, China)
Jinwu Xiang (School of Aeronautic Science and Engineering, Beihang University, Beijing, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 29 March 2024

Issue publication date: 16 April 2024

117

Abstract

Purpose

The purpose of this paper is to solve the challenging problem of automatic carrier landing with the presence of environmental disturbances. Therefore, a global fast terminal sliding mode control (GFTSMC) method is proposed for automatic carrier landing system (ACLS) to achieve safe carrier landing control.

Design/methodology/approach

First, the framework of ACLS is established, which includes flight glide path model, guidance model, approach power compensation system and flight controller model. Subsequently, the carrier deck motion model and carrier air-wake model are presented to simulate the environmental disturbances. Then, the detailed design steps of GFTSMC are provided. The stability analysis of the controller is proved by Lyapunov theorems and LaSalle’s invariance principle. Furthermore, the arrival time analysis is carried out, which proves the controller has fixed time convergence ability.

Findings

The numerical simulations are conducted. The simulation results reveal that the proposed method can guarantee a finite convergence time and safe carrier landing under various conditions. And the superiority of the proposed method is further demonstrated by comparative simulations and Monte Carlo tests.

Originality/value

The GFTSMC method proposed in this paper can achieve precise and safe carrier landing with environmental disturbances, which has important referential significance to the improvement of ACLS controller designs.

Keywords

Acknowledgements

This work was supported by the National Natural Science Foundation of China (No. T2288101) and the National Key Research and Development Project (No. 2020YFC1512500).

This research was funded by the National Natural Science Foundation of China, grant number 11972059.

Conflict of interests: The authors declare no conflict of interest.

Citation

Yao, Z., Kan, Z., Li, D., Shao, H. and Xiang, J. (2024), "Global fast terminal sliding mode control for automatic carrier landing with environmental disturbances", Aircraft Engineering and Aerospace Technology, Vol. 96 No. 3, pp. 465-474. https://doi.org/10.1108/AEAT-10-2023-0273

Publisher

:

Emerald Publishing Limited

Copyright © 2024, Emerald Publishing Limited

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